Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11986
Days in orbit
Revolutions
≈ 14.4
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.0
Latest
Satellite identification and parameters
Extended collection of information and parameters for SL-16 DEB.
Object identification
Identified? True
Debris? True
Object name: SL-16 DEB
International designator: 1992-093CW
Object number (NORAD): 22405
Object ID (CCSDS): 22405
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 99.838 minutes
Inclination: 71.0358 deg
SMA: 7128.94 km
Apoapsis: 839.805 km
Periapsis: 661.805 km
RAAN: 58.7534 deg
Eccentricy: 0.01248433
Argument of periapsis: 258.127 deg
Mean anomaly: 100.5845 deg
Mean motion: 14.42332374 rev/day
Mean motion (dot): 0.00000943 rev/day2
B* drag term: 0.00027554834 1/REarth
Two-line elements (TLE)
Creation date: Oct. 19, 2025, 2:20 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 18, 2025, 3:57 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22405U 92093CW 25291.66521323 .00000943 00000-0 27555-3 0 9996
TLE line 2: 2 22405 71.0358 58.7534 0124843 258.1270 100.5845 14.42332374699750
Live tracking on map
Real-time ground track for satellite SL-16 DEB.
Associated space launch
Second generation ELING satellite
SL-16 DEB was lifted into orbit during the mission ‘Zenit-2 | Tselina-2 12’, on board a Zenit-2 space rocket.
The launch took place on Dec. 25, 1992, 5:56 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 12
Agency: N/A
Status: Launch Successful
Launch date: Dec. 25, 1992, 5:56 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
...
Latest news about this satellite
There are no fresh news available about this satellite. Check back as we update our databases every day.
Newsletter sign-up
Weekly statistics, charts and insights to help you stay on top of the space industry.
